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Multi GNSS Current Status and Futurefig.net/pub/fig2012/ppt/iag/session2_3_3_hothem.pdf · 2012. 6....

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Multi GNSS Current Status and Future Session 2.3 Multi GNSS Environment Larry D. Hothem Senior Advisor for GPS/GNSS Technical Issues Member US Delegation to the ICG DOI Lead Member, GPS International Working Group (GIWG), PNT DOI Member of Various PNT Working Groups U.S. Geological Survey, Department of the Interior Reston, Virginia USA
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  • Multi GNSS

    Current Status and Future

    Session 2.3 Multi GNSS Environment

    Larry D. Hothem

    Senior Advisor for GPS/GNSS Technical Issues

    Member US Delegation to the ICG

    DOI Lead Member, GPS International Working Group (GIWG), PNT

    DOI Member of Various PNT Working Groups

    U.S. Geological Survey, Department of the Interior

    Reston, Virginia USA

  • • GNSS

    • GPS Performance and Modernization

    • Multi-GNSS and Reference Frame Issues

    • GNSS Signal Interfernce and Detection

    – LightSquared Matter - Status

  • 3

    U.S. Space-Based PNTOrganization Structure

    WHITE HOUSE

    ADVISORY BOARD

    Sponsor: NASA

    NATIONALEXECUTIVE COMMITTEEFOR SPACE-BASED PNT

    Executive Steering Group

    Co-Chairs: Defense, Transportation

    NATIONAL COORDINATION OFFICE

    Host: Commerce

    GPS International Working Group

    Chair: State

    Engineering Forum

    Co-Chairs: Defense, Transportation

    Ad HocWorking Groups

    Defense

    Transportation

    State

    Interior

    Agriculture

    Commerce

    Homeland Security

    Joint Chiefs of Staff

    NASA

    http://pnt.gov/membership/http://pnt.gov/advisory/http://pnt.gov/http://pnt.gov/office/http://pnt.gov/groups/http://pnt.gov/groups/http://pnt.gov/membership/dod.shtmlhttp://pnt.gov/membership/dot.shtmlhttp://pnt.gov/membership/dos.shtmlhttp://pnt.gov/membership/doi.shtmlhttp://pnt.gov/membership/usda.shtmlhttp://pnt.gov/membership/doc.shtmlhttp://pnt.gov/membership/dhs.shtmlhttp://pnt.gov/membership/jcs.shtmlhttp://pnt.gov/membership/nasa.shtml

  • Signals of GNSS Open Services

  • Signal spectra for GPS, Galileo, Compass, and GLONASS. From the left, new GPS satellites radiate at L5 (1176.45 MHz), L2 (1227.60 MHz), and L1 (1575.42 MHz)

  • GPS Enterprise View Civil

    Cooperation •1+ Billion civil &

    commercial users

    •Search and Rescue

    •Civil Signals

    - L2C (2nd Civil

    Signal)

    - L5 (Safety of Life)

    - L1C (International)

    Spectrum

    •World Radio Conference

    •International

    Telecommunication

    Union

    •Bilateral Agreements

    International Cooperation •Deconflict PRN usage for 8 global

    PNT systems

    - 63 for US and 147 for other GNSS

    • 25+ Years of Cooperation with

    50+ Nations

    •GNSS

    - China – COMPASS (BeiDou)

    - Europe – Galileo/EGNOS

    - India – IRNSS/GAGAN

    - Japan – QZSS/MSAS

    - Russia – GLONASS/SDCM

    Dual Use Management

    • Department of Defense Services (Army, Navy, AF,

    USMC)

    • Agencies (NGA, DISA,

    etc.)

    • US Naval Observatory

    • Department of

    Transportation

    • PNT EXCOMS, NPEF, etc

    • GPS Partnership Council

    34 Satellites/ 31 Set Healthy

    Baseline Constellation: 24 Satellites

    Satellite Quantity Avg

    Life

    Oldest

    GPS IIA 10 18.0 21.3

    GPS IIR 12 10.2 14.6

    GPS IIR-M 7 4.6 6.4

    GPS IIF 2 1.2 1.8

    Constellation 31 10.9 21.3

  • GPS Constellation Status

    • 10 Block IIA Satellites

    • 12 Block IIR Satellites

    • 7 Block IIR-M Satellites

    • 2 Block IIF Satellites

    – IIF-2 healthy as of October 16, 2011

    – Next IIF launch scheduled mid-2012

    • Global GPS civil service performance commitment met continuously since December 1993

    31 Healthy SatellitesBaseline Constellation: 24 + 3

    8

  • Standard Positioning Service (SPS)Signal-in-Space Performance

    1.61.4

    1.2 1.2 1.1 1.1 1.0 1.0 0.9 0.9

    0

    1

    2

    3

    4

    5

    6

    7

    8

    2001 2002 2003 2004 2005 2006 2007 2008 2009 2010

    Ro

    ot

    Me

    an

    Sq

    ua

    re (

    RM

    S)

    Sig

    na

    l-in

    -Sp

    ace

    (S

    IS)

    Use

    r R

    an

    ge

    Err

    or

    (UR

    E)

    in m

    ete

    rs 2001 SPS Performance Standard

    (6.0 m RMS overall SPS SIS URE)

    2008 SPS Perform. Standard

    (4.0 m RMS worst of any SPS SIS URE)

    Signal-in-Space User Range Error is the difference between a GPS satellite’s navigation data (position and clock) and the truth, projected on the line-of-sight to the user

    System accuracy exceeds published standard

    9

  • Civil Capability Improvements

    Second civil signal “L2C”

    • Designed to meet commercial needs

    • Higher accuracy through ionospheric correction

    • Available since 2005 without data message– Currently, 7 IIR-Ms transmitting L2C

    • Full capability: 24 satellites ~2016

    Third civil signal “L5”

    • Designed to meet demanding requirements for transportation safety

    • Uses highly protected Aeronautical Radio Navigation Service (ARNS) band

    • Operational on 2 GPS IIF satellites

    • Full capability: 24 satellites ~2018

    After 2020, with L2C and L5 online, the USG will no longer support semi-codeless access to military GPS signals

  • Civil Capability Improvements

    Fourth civil signal “L1C”

    • Designed with international partnersfor interoperability

    • Modernized civil signal at L1 frequency

    – More robust navigation across a broad range of user applications

    – Improved performance in challengedtracking environments

    – Original signal retained for backward compatibility

    • Specification developed in cooperation with industry

    • Launches with GPS III in 2014

    • On 24 satellites by ~2021

    Under Trees

    Urban Canyons

  • Patent Issue on L1C

  • GPS IIR/IIR-M Status

    • All GPS IIR and IIR-M satellites are on orbit

    – Current backbone of the GPS constellation

    • Excellent on-orbit performance

    – SIS URE of .50 meters (1 yr performance Jul 11)

    • Excellent life expectancy

    – Solar array capacity far exceeds specification

    – No clock failures to date

  • GPS IIF Status

    • On-orbit performance for IIF-1

    – SIS URE of .30 meters (1 yr performance Jul 11)

    • Launched GPS IIF-2 on 15 Jul 11

    – SVN 63, PRN 1

    – Set healthy 14 October 2011

    – Second operational L5

    – Increases the enhanced GPS clockperformance coverage

    • 10 more IIFs in the pipeline

    – SVs 3-8 are in Assembly, Integration & Test

    • IIF-3 launch scheduled Sept. 2012

  • GPS III Status

    • Newest block of GPS satellites

    – First GPS satellite to broadcast L1C signal

    – Multiple civil and military signals; L1 C/A,L1 P(Y), L1M, L1C, L2C, L2 P(Y), L2M, L5

    – Three Rubidium clocks

    • Completed Critical Design Review

    • Prototype and engineering unit build/test underway

    – Completed 57 of 59 Manufacturing Readiness Reviews

    – Completed 43 of 59 Test Readiness Reviews

    • GPS Nonflight Satellite Testbed (GNST) integration

    underway

    • Initiated Capability Insertion Program for SV-9+

  • GPS Modernization Program

    Increasing System Capabilities w Increasing User Benefit

    Block IIA/IIR Block IIIBlock IIR-M, IIF

    • Backward compatibility

    • 4th civil signal (L1C)

    • Improved User Range Error

    • Increased availability

    • Increased integrity

    • 15 year design life

    IIR-M – Basic GPS capability plus

    • 2nd civil signal (L2C)

    • M-Code (L1M & L2M)

    IIF – IIR-M capability plus

    • 3rd civil signal (L5)

    • 2 Rb + 1 Cs Clocks

    • 12 year design life

    Basic GPS

    • Standard Service

    – Single frequency (L1)

    – Coarse acquisition (C/A) code navigation

    • Precise Service

    – Y-Code (L1Y & L2Y)

    – Y-Code navigation

    16

  • GPS Modernization Program

    17

    Block I Block II/IIA Block IIR Block IIR-M Block IIF Block III

    • L1 (CA) Navigation signal

    • L1 & L2 (P Code) Navigation signal

    • 5 Year Design Life

    • Standard Service • Single Frequency (L1)• C/A code navigation• Precise Service • Two frequencies (L1 & L2)• P (Y) -Code navigation• 7.5 Year Design Life

    Demonstration system

    Basic GPSProvides Initial Navigation Capabilities

    IIA/IIR Capabilities “Plus”

    • 2nd Civil Signal L2 (L2C)

    • Earth Coverage M-Code on L1/L2

    • L5 Demo• Anti-Jam Flex

    Power• 7.5 Year Design

    Life

    IIR -M Capabilities “Plus”

    • 3rd Civil Signal L5• Reprogrammable

    Nav Processer • Increased Accuracy

    requirement• 12 Year Design Life

    IIF Capabilities “Plus”

    IIIA• Increased accuracy• Increased Earth

    Coverage power• 15 Year Design Life• 4th Civil Signal (L1C)

    IIIB• near-real-time

    commanding

    IIIC• Navigation Integrity• Spot Beam for AJ

    1978 - 1985 1989 – 1997 1997- 2004 2005 - 2009 2010 - Present 2014 – 2024

    11 (10) Satellites 28 Satellites 13 (12) Satellites 8 Satellites 12 Satellites 32 Satellites

    Increasing Space System Capabilities – Increasing Military/Civil User Benefits

  • Control Segment Status

    • Operational Control Segment (OCS)

    – Now flying Block IIA/IIR/IIR-M/IIF constellation

    – Added the capability for anomaly resolution and disposal ops for IIF

    • Next Generation Operational Control System (OCX)

    – Preliminary Design Review concluded August 2011

    – OCX Block I deployment planned for August 2015

    – New Launch and Checkout System will control first GPS III satellites prior to OCX Block I

    Monitor Station Ground Antenna

    Master Control Stations at

    Schriever AFB, Colorado

  • GPS Status Summary

    19

    • GPS has continuously met its

    commitments to all users

    • Modernization of all GPS

    Segments is on track

    • Striving to continually

    improve navigation and timing

    services while maintaining

    backward compatibility with

    legacy equipment

    • GPS is committed to open

    and transparent cooperation

    with the international GNSS

    community

  • Receivers track four different GPS satellite types

    Reference frame issues

  • In the future, GNSS may grow to include more than 100 satellites, mostly in medium Earth orbit, with

    some in geostationary and inclined elliptical orbits

    Multi-GNSS

  • Transparent multi-GNSS interoperability is achievable through system and receiver design.

    Reference frame issues

  • Possible Framework of International Multi-GNSS Service

  • GNSS Signal Interference and Detection

    24

  • Personal protection devices (PPDs)

  • Example of a personal privacy device (PPD)

  • Harmonics May Interfere with GPS L1 Band

  • LightSquared Matter

    29

    • Created 2010 (previously known as “SkyTerra”)

    – Mobile satellite service (MSS) licensee in the 1525-1559 MHz/1626.5-1660.5 MHz band

    – Authorized in 2003 to operate ancillary terrestrial component (ATC) as satellite “fill-in”

    • Required dual-mode MSS/ATC devices to meet gating criteria

    – LightSquared’s goal is to build out a nationwide 4G broadband network (to cover 92% of USA by 2015)

    • Nov 18, 2010 – Request submitted to FCC for modification of its ATC authority

    • Jan 26, 2011 – FCC Order & Authorization

    – Granted conditional waiver (ATC-only handsets)

    – Requires resolving GPS concerns before commencing commercial operations

  • Illustration of Concernswith LightSquared

    GLONASS

    GLONASS

    1525 1559 1575 1610

    Situation before LightSquared

    1525 1559 1575 1610

    Situation with LightSquared

    low power (on Earth) satcom emissions

    low power (on Earth) satcom emissions

    30

    Up to 15 kW base

    station emissions

  • 1525 1559 1610

    L Band Satellite Downlink (34 MHz) RNSS band (GPS, 51MHz)

    LTE (10) LTE (10)1526 1536 1545.2 1555.2

    3.89.2

    LTE (5)1526.3 1531.3

    LTE (5)

    1550.2 1555.2

    1575.42 MHz

    16.42 MHz

    L1

    Phase 0/1

    Phase 2

    1525 1559 1626.51610

    L Band Satellite

    (Uplink)

    L Band Satellite

    (Downlink)

    Ae

    ron

    au

    tica

    l

    Te

    lem

    etr

    y

    Aeronautical Radio navigation/

    Radio navigation-Satellite

    (GPS, 51MHz)

    Big LEO

    (Uplink)

    1660.5

    Original LightSquared Spectrum Plan

    31

  • Javad Filter Response to Mitigate theLower 10 MHz LightSquared Signal

    32

  • LightSquared (LSQ)

    – Testing of LSQ signal directly adjacent to GPS from LSQ towers to identify impact on the GPS signal

    • Testing conclusively showed that the LSQ’s signal interfered directly with GPS receiver operation

    – On February 14, 2012 the FCC rescinded the “Conditional Waiver Order” to continue to protect GPS receiver operation

    – Federal Communications Commission (FCC) Office of Engineering and Technology is reviewing spectrum efficiency and receivers

    • This is to enhance the use of spectrum for mobile broadband without affecting the GPS spectrum

    – U.S. Department of Transportation and Commerce Department's National Telecommunications and Information Administration (NTIA)

    • NTIA is the other U.S. organization that manages government spectrum

    • U.S. interagency working to draft new GPS spectrum-interference standards to further strengthen existing policy protection of GPS

  • Summary on LightSquared

    • LightSquared signals caused harmful interference to majority of GPS receivers tested

    – With exception of cellular phones, Lower 10 MHz does not solve the problem, particularly with high-precision receivers

    • Even an acceptable filter solution would need a long term transition/implementation plan to protect legacy GPS service and users (similar to semi-codeless GPS or analog to digital TV)

    34

  • THANK YOU


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